A shock wave detection system includes a light beam emitter, a light beam receiver and an analysis unit. The light beam emitter emits a light beam oblique to a direction of an air flow through which a shock wave may propagate. The light beam receiver receives the light beam that has passed through the air flow. The analysis unit is configured to detect a presence and a position of the shock wave based on a change in a receiving position of the light beam by the light beam receiver.
SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT
2024-03-28
Patent
Electronic Resource
English
SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT
SAE Technical Papers | 1960
|Shock wave noise of supersonic aircraft
Engineering Index Backfile | 1960
|